Self-lubricating bush assembly

US11293495B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-11293495-B2
Application numberUS-202016898878-A
CountryUS
Kind codeB2
Filing dateJun 11, 2020
Priority dateJun 14, 2019
Publication dateApr 5, 2022
Grant dateApr 5, 2022

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  1. Title

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  2. Abstract

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  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

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  6. CPC / IPC classifications

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  7. Citations and related patents

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Abstract

Official abstract text for this publication.

A bush assembly configured to be disposed between a first component and a second component movably coupled to the first component, the bush assembly comprising a first bush portion comprising a self-lubricating material; and a second bush portion, the second bush portion having greater electrical conductivity than the first bush portion, wherein the second bush portion provides a conductive path between the first component and the second component.

First claim

Opening claim text (preview).

The invention claimed is: 1. A bush assembly configured to be disposed between a first component and a second component movably coupled to the first component, the bush assembly comprising: a first bush portion comprising a self-lubricating material; and a second bush portion, the second bush portion having greater electrical conductivity than the first bush portion, wherein the second bush portion provides a conductive path between the first component and the second component, and the second bush portion is removable from the first bush portion, and wherein a cross-sectional shape of the second bush provides for elastic deformation. 2. The bush assembly according to claim 1 , wherein the second bush portion comprises any of an electrically conductive elastomer, graphite, or a metallic material. 3. The bush assembly according to claim 1 , further comprising a third bush portion comprising the self-lubricating material, wherein the second bush portion is located between the first bush portion and third bush portion. 4. The bush assembly according to claim 3 , wherein the second bush portion is configured to exert a force on at least one of the first bush portion and the third bush portion. 5. The bush assembly according to claim 1 further comprising at least one flange attached to at least one of the first bush portion and the second bush portion. 6. The bush assembly according to claim 1 , wherein the second bush portion is configured to exert a force on at least one of the first component and the second component. 7. The bush assembly according to claim 6 , wherein the second bush portion is assembled in the bush assembly in a compressed state to thereby generate the force. 8. The bush assembly according to claim 1 , wherein the first bush portion and the second bush portion each has a respective inner surface in contact with the first component, and a respective outer surface in contact with the second component. 9. A joint assembly comprising: a first component; a second component movably coupled to the first component; and a bush assembly disposed between the first component and the second component, the bush assembly comprising: a first bush portion comprising a self-lubricating material; and a second bush portion, the second bush portion having greater electrical conductivity than the first bush portion, wherein the second bush portion provides a conductive path between the first component and the second component, the second bush portion is removable from the first bush portion, and wherein a cross-sectional shape of the second bush provides for elastic deformation. 10. The joint assembly according to claim 9 , wherein the first component is a joint pin and the second component is pivotally coupled to the joint pin. 11. The joint assembly according to claim 9 , wherein the first component is a shaft, the shaft being coupled to the second component so that the shaft can move relative to the second component along a longitudinal axis of the shaft. 12. An aircraft landing gear assembly comprising one or more joint assemblies according to claim 9 . 13. An aircraft comprising one or more aircraft landing gear assemblies according to claim 12 .

Assignees

Inventors

Classifications

  • Sliding surface consisting mainly of graphite · CPC title

  • Brasses; Bushes; Linings · CPC title

  • Lightning protectors; Static dischargers · CPC title

  • retractable, foldable, or the like · CPC title

  • Lubrication with substances other than oil or grease; Lubrication characterised by the use of particular lubricants in particular apparatus or conditions (F16N17/00 takes precedence; lubricating compositions, selection of particular substances as lubricants in general C10M) · CPC title

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What does patent US11293495B2 cover?
A bush assembly configured to be disposed between a first component and a second component movably coupled to the first component, the bush assembly comprising a first bush portion comprising a self-lubricating material; and a second bush portion, the second bush portion having greater electrical conductivity than the first bush portion, wherein the second bush portion provides a conductive pat…
Who is the assignee on this patent?
Safran Landing Systems Uk Ltd
What technology area does this patent fall under?
Primary CPC classification F16C33/24. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Apr 05 2022 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 4 related publications on this page (citations in our corpus or others sharing the same primary CPC).